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FX 84-W-097 (fx84w097-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 84-W-097 (fx84w097-il)
Reynolds number: 1,000,000
Max Cl/Cd: 123.64 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx84w097-il-1000000.txt
Download as CSV file: xf-fx84w097-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 84-W-097                                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.4001   0.12920   0.12775  -0.0018   1.0000   0.0118
 -12.000  -0.4027   0.12380   0.12236  -0.0036   1.0000   0.0122
  -9.750  -0.7335   0.03041   0.02801  -0.0555   0.9829   0.0090
  -9.500  -0.7145   0.02766   0.02496  -0.0568   0.9536   0.0092
  -9.250  -0.7037   0.02549   0.02248  -0.0554   0.9308   0.0094
  -9.000  -0.6871   0.02406   0.02083  -0.0544   0.9155   0.0096
  -8.750  -0.6703   0.02215   0.01863  -0.0535   0.9026   0.0097
  -8.500  -0.6512   0.02047   0.01667  -0.0528   0.8915   0.0099
  -8.250  -0.6302   0.01905   0.01501  -0.0522   0.8816   0.0102
  -8.000  -0.6082   0.01775   0.01346  -0.0516   0.8722   0.0104
  -7.750  -0.5847   0.01662   0.01214  -0.0512   0.8632   0.0108
  -7.500  -0.5605   0.01567   0.01098  -0.0507   0.8550   0.0111
  -7.250  -0.5350   0.01501   0.01017  -0.0505   0.8466   0.0115
  -7.000  -0.5083   0.01477   0.00983  -0.0503   0.8389   0.0118
  -6.750  -0.4860   0.01289   0.00768  -0.0497   0.8308   0.0128
  -6.500  -0.4596   0.01240   0.00712  -0.0495   0.8235   0.0134
  -6.250  -0.4329   0.01200   0.00663  -0.0494   0.8157   0.0140
  -6.000  -0.4059   0.01159   0.00615  -0.0492   0.8082   0.0148
  -5.750  -0.3789   0.01122   0.00568  -0.0491   0.8006   0.0155
  -5.500  -0.3512   0.01099   0.00539  -0.0490   0.7933   0.0161
  -5.250  -0.3257   0.01012   0.00438  -0.0487   0.7860   0.0178
  -5.000  -0.2981   0.00985   0.00408  -0.0486   0.7790   0.0190
  -4.750  -0.2704   0.00966   0.00384  -0.0486   0.7717   0.0205
  -4.500  -0.2424   0.00951   0.00365  -0.0486   0.7649   0.0216
  -4.250  -0.2155   0.00898   0.00303  -0.0484   0.7578   0.0244
  -4.000  -0.1876   0.00878   0.00280  -0.0484   0.7510   0.0268
  -3.750  -0.1595   0.00866   0.00264  -0.0484   0.7438   0.0288
  -3.500  -0.1319   0.00832   0.00228  -0.0483   0.7371   0.0339
  -3.250  -0.1038   0.00818   0.00210  -0.0483   0.7297   0.0377
  -3.000  -0.0759   0.00796   0.00187  -0.0483   0.7228   0.0460
  -2.750  -0.0478   0.00779   0.00171  -0.0484   0.7154   0.0564
  -2.500  -0.0198   0.00762   0.00157  -0.0484   0.7084   0.0708
  -2.250   0.0083   0.00746   0.00145  -0.0485   0.7009   0.0906
  -2.000   0.0363   0.00729   0.00134  -0.0485   0.6941   0.1186
  -1.750   0.0643   0.00710   0.00125  -0.0486   0.6867   0.1537
  -1.500   0.0921   0.00689   0.00117  -0.0487   0.6801   0.2044
  -1.250   0.1199   0.00663   0.00110  -0.0488   0.6729   0.2691
  -1.000   0.1472   0.00627   0.00104  -0.0489   0.6661   0.3746
  -0.750   0.1740   0.00580   0.00099  -0.0490   0.6589   0.5168
  -0.500   0.1998   0.00533   0.00098  -0.0487   0.6522   0.6777
  -0.250   0.2257   0.00505   0.00101  -0.0482   0.6450   0.7800
   0.000   0.2519   0.00496   0.00104  -0.0477   0.6380   0.8348
   0.250   0.2779   0.00490   0.00106  -0.0471   0.6303   0.8747
   0.500   0.3035   0.00489   0.00109  -0.0463   0.6229   0.9053
   0.750   0.3288   0.00488   0.00111  -0.0455   0.6150   0.9310
   1.000   0.3548   0.00490   0.00112  -0.0449   0.6076   0.9515
   1.250   0.3837   0.00492   0.00113  -0.0450   0.5998   0.9688
   1.500   0.4180   0.00497   0.00114  -0.0463   0.5922   0.9832
   1.750   0.4562   0.00501   0.00115  -0.0485   0.5837   0.9914
   2.000   0.4977   0.00506   0.00116  -0.0515   0.5741   0.9987
   2.250   0.5264   0.00513   0.00119  -0.0518   0.5646   1.0000
   2.500   0.5518   0.00521   0.00123  -0.0513   0.5553   1.0000
   2.750   0.5778   0.00528   0.00129  -0.0510   0.5470   1.0000
   3.000   0.6041   0.00539   0.00135  -0.0507   0.5376   1.0000
   3.250   0.6310   0.00547   0.00141  -0.0505   0.5275   1.0000
   3.500   0.6581   0.00556   0.00149  -0.0504   0.5178   1.0000
   3.750   0.6852   0.00568   0.00158  -0.0503   0.5070   1.0000
   4.000   0.7122   0.00582   0.00166  -0.0502   0.4877   1.0000
   4.250   0.7389   0.00601   0.00177  -0.0501   0.4634   1.0000
   4.500   0.7657   0.00621   0.00190  -0.0500   0.4413   1.0000
   4.750   0.7925   0.00641   0.00204  -0.0499   0.4221   1.0000
   5.000   0.8191   0.00666   0.00220  -0.0498   0.3962   1.0000
   5.250   0.8450   0.00698   0.00239  -0.0496   0.3639   1.0000
   5.500   0.8703   0.00739   0.00264  -0.0494   0.3241   1.0000
   5.750   0.8943   0.00796   0.00297  -0.0491   0.2700   1.0000
   6.000   0.9171   0.00868   0.00339  -0.0486   0.2094   1.0000
   6.250   0.9390   0.00948   0.00387  -0.0481   0.1476   1.0000
   6.500   0.9604   0.01033   0.00442  -0.0474   0.0917   1.0000
   6.750   0.9832   0.01097   0.00489  -0.0469   0.0606   1.0000
   7.000   1.0066   0.01151   0.00533  -0.0465   0.0425   1.0000
   7.250   1.0302   0.01201   0.00577  -0.0460   0.0313   1.0000
   7.500   1.0541   0.01245   0.00620  -0.0456   0.0254   1.0000
   7.750   1.0778   0.01291   0.00667  -0.0451   0.0211   1.0000
   8.000   1.0999   0.01350   0.00726  -0.0444   0.0173   1.0000
   8.250   1.1232   0.01394   0.00773  -0.0439   0.0158   1.0000
   8.500   1.1461   0.01440   0.00821  -0.0433   0.0143   1.0000
   8.750   1.1671   0.01502   0.00887  -0.0425   0.0130   1.0000
   9.000   1.1846   0.01592   0.00987  -0.0412   0.0120   1.0000
   9.250   1.2061   0.01640   0.01039  -0.0404   0.0115   1.0000
   9.500   1.2258   0.01698   0.01103  -0.0394   0.0110   1.0000
   9.750   1.2454   0.01753   0.01162  -0.0385   0.0104   1.0000
  10.000   1.2630   0.01819   0.01231  -0.0373   0.0100   1.0000
  10.250   1.2786   0.01892   0.01310  -0.0358   0.0095   1.0000
  10.500   1.2863   0.01995   0.01420  -0.0331   0.0091   1.0000
  10.750   1.2809   0.02160   0.01600  -0.0289   0.0086   1.0000
  11.000   1.2899   0.02257   0.01704  -0.0269   0.0085   1.0000
  11.250   1.3026   0.02335   0.01788  -0.0254   0.0082   1.0000
  11.500   1.3090   0.02466   0.01927  -0.0235   0.0081   1.0000
  11.750   1.3189   0.02575   0.02044  -0.0221   0.0079   1.0000
  12.000   1.3271   0.02706   0.02183  -0.0207   0.0076   1.0000
  12.250   1.3328   0.02863   0.02349  -0.0193   0.0075   1.0000
  12.500   1.3416   0.02999   0.02493  -0.0183   0.0073   1.0000
  12.750   1.3483   0.03158   0.02660  -0.0173   0.0071   1.0000
  13.000   1.3555   0.03318   0.02827  -0.0165   0.0069   1.0000
  13.250   1.3613   0.03497   0.03012  -0.0158   0.0067   1.0000
  13.500   1.3651   0.03702   0.03225  -0.0152   0.0065   1.0000
  13.750   1.3649   0.03956   0.03489  -0.0146   0.0063   1.0000
  14.000   1.3597   0.04278   0.03824  -0.0141   0.0061   1.0000
  14.250   1.3483   0.04687   0.04251  -0.0136   0.0060   1.0000
  14.500   1.3439   0.05030   0.04609  -0.0137   0.0059   1.0000
  14.750   1.3385   0.05394   0.04987  -0.0140   0.0059   1.0000
  15.000   1.3410   0.05675   0.05279  -0.0147   0.0058   1.0000
  15.250   1.3397   0.06019   0.05635  -0.0155   0.0057   1.0000
  15.500   1.3338   0.06443   0.06073  -0.0167   0.0057   1.0000
  15.750   1.3306   0.06843   0.06485  -0.0181   0.0056   1.0000
  16.000   1.3261   0.07280   0.06935  -0.0198   0.0055   1.0000
  16.250   1.3153   0.07834   0.07505  -0.0221   0.0055   1.0000
  16.500   1.3057   0.08393   0.08079  -0.0246   0.0055   1.0000
  16.750   1.2932   0.09032   0.08733  -0.0276   0.0054   1.0000
  17.000   1.2801   0.09701   0.09417  -0.0311   0.0054   1.0000
  17.250   1.2644   0.10458   0.10191  -0.0351   0.0053   1.0000
  17.500   1.2495   0.11219   0.10965  -0.0393   0.0054   1.0000
  17.750   1.2327   0.12057   0.11819  -0.0442   0.0053   1.0000
  18.000   1.2123   0.13010   0.12787  -0.0499   0.0054   1.0000
  18.250   1.1924   0.13999   0.13791  -0.0559   0.0054   1.0000
  18.500   1.1693   0.15111   0.14918  -0.0628   0.0055   1.0000
  18.750   1.1363   0.16578   0.16403  -0.0718   0.0056   1.0000
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